[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 5th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 123 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 362 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 1844)
---------------------------------------
Vector Time (GMT): 2013/063/12:20:01
915
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2094555
03 A = 6791766
81 meter
Y = -6041535
13 meter E =
0015312
Z = -2260520
39 I = 51
30398
XDOT = 4180
907871 Wp = 356
80751
YDOT = -3470
857783 meter/sec RA = 267
32920 deg
ZDOT = 5415
604614 TA = 337
91167
MA = 337
97758
Ha = 225
489 n
mi
Hp = 217
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6871899
71 X = -2015860
71
Y = -19821309
47 feet Y = -6064517
89 meter
Z = -7416405
47 Z = -2270503
96
XDOT = 13716
889339 XDOT = 4193
101652
YDOT = -11387
328683 feet/sec YDOT = -3424
035736 meter/sec
ZDOT = 17767
731674 ZDOT = 5435
944768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2054678
38 X = -626265
97
Y = -20863325
39 feet Y = -6359141
58 meter
Z = -7457233
75 Z = -2272964
85
XDOT = 14350
893790 XDOT = 4374
152427
YDOT = -7779
036750 feet/sec YDOT = -2371
050401 meter/sec
ZDOT = 17852
749752 ZDOT = 5441
518124
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13063
51842968
00016717 00000-0 10270-3 0 9003
2 25544 51
6444 268
1457 0012103 335
7391 24
3189 15
52538071 18459
Satellite: ISS
Catalog Number: 25544
Epoch time: 13063
51842968 = yrday
fracday
Element set: 900
Inclination: 51
6444 deg
RA of node: 268
1457 deg
Eccentricity:
0012103
Arg of perigee: 335
7391 deg
Mean anomaly: 24
3189 deg
Mean motion: 15
52538071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1845
Checksum: 306
Coasting Arc #2 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2013/064/12:20:01
915
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1773851
35 A = 6793214
66 meter
Y = 6463062
77 meter E =
0008341
Z = 1119695
09 I = 51
31210
XDOT = -4420
218142 Wp = 59
85511
YDOT = 2231
642044 meter/sec RA = 262
34107 deg
ZDOT = -5841
886529 TA = 107
95757
MA = 107
86663
Ha = 225
699 n
mi
Hp = 216
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5819722
27 X = 1696009
05
Y = 21204274
18 feet Y = 6482463
91 meter
Z = 3673540
33 Z = 1128122
78
XDOT = -14502
028026 XDOT = -4416
466338
YDOT = 7321
660249 feet/sec YDOT = 2182
233044 meter/sec
ZDOT = -19166
294387 ZDOT = -5863
350312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1111412
78 X = 338758
61
Y = 21954540
83 feet Y = 6691744
04 meter
Z = 3707857
62 Z = 1130155
00
XDOT = -14018
476290 XDOT = -4272
831573
YDOT = 3981
992151 feet/sec YDOT = 1213
711208 meter/sec
ZDOT = -19255
845897 ZDOT = -5869
181829
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13064
54830901
00016717 00000-0 10270-3 0 9012
2 25544 51
6446 263
0241 0012329 339
8184 20
2479 15
52605299 18613
Satellite: ISS
Catalog Number: 25544
Epoch time: 13064
54830901 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 263
0241 deg
Eccentricity:
0012329
Arg of perigee: 339
8184 deg
Mean anomaly: 20
2479 deg
Mean motion: 15
52605299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 299
Coasting Arc #3 (Orbit 1876)
---------------------------------------
Vector Time (GMT): 2013/065/12:20:01
915
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1436455
20 A = 6793891
49 meter
Y = -6626029
83 meter E =
0020756
Z = 61282
11 I = 51
31764
XDOT = 4700
543421 Wp = 14
93534
YDOT = -959
610850 meter/sec RA = 257
35350 deg
ZDOT = 5990
912069 TA = 345
72806
MA = 345
78661
Ha = 225
789 n
mi
Hp = 216
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4712779
52 X = -1362552
45
Y = -21738943
02 feet Y = -6641679
96 meter
Z = 201056
79 Z = 54483
96
XDOT = 15421
730383 XDOT = 4681
822870
YDOT = -3148
329561 feet/sec YDOT = -907
150725 meter/sec
ZDOT = 19655
223323 ZDOT = 6013
701109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -321564
74 X = -98012
93
Y = -22241826
44 feet Y = -6779308
70 meter
Z = 173524
84 Z = 52890
37
XDOT = 13998
527851 XDOT = 4266
751289
YDOT = -35
439970 feet/sec YDOT = -10
802103 meter/sec
ZDOT = 19750
147580 ZDOT = 6019
844982
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13065
57817936
00016717 00000-0 10270-3 0 9020
2 25544 51
6433 257
9009 0012105 343
5906 16
4853 15
52563556 18778
Satellite: ISS
Catalog Number: 25544
Epoch time: 13065
57817936 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 257
9009 deg
Eccentricity:
0012105
Arg of perigee: 343
5906 deg
Mean anomaly: 16
4853 deg
Mean motion: 15
52563556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1877
Checksum: 322
Coasting Arc #4 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2013/066/12:20:01
915
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1033279
14 A = 6793017
44 meter
Y = 6597254
35 meter E =
0005636
Z = -1266244
60 I = 51
32294
XDOT = -4981
203062 Wp = 30
92497
YDOT = -332
602343 meter/sec RA = 252
36769 deg
ZDOT = -5804
464940 TA = 162
88146
MA = 162
86244
Ha = 225
953 n
mi
Hp = 216
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3390023
42 X = 965581
40
Y = 21644535
26 feet Y = 6608430
51 meter
Z = -4154345
81 Z = -1261390
06
XDOT = -16342
529730 XDOT = -4948
917638
YDOT = -1091
215036 feet/sec YDOT = -388
125219 meter/sec
ZDOT = -19043
520143 ZDOT = -5828
584264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -555709
06 X = -169380
12
Y = 21905037
84 feet Y = 6676655
53 meter
Z = -4134883
22 Z = -1260312
41
XDOT = -14162
232138 XDOT = -4316
648356
YDOT = -3968
706191 feet/sec YDOT = -1209
661647 meter/sec
ZDOT = -19143
840709 ZDOT = -5835
042648
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13066
54366876
00016717 00000-0 10270-3 0 9031
2 25544 51
6432 253
0992 0012234 347
6775 12
4076 15
52626802 18921
Satellite: ISS
Catalog Number: 25544
Epoch time: 13066
54366876 = yrday
fracday
Element set: 903
Inclination: 51
6432 deg
RA of node: 253
0992 deg
Eccentricity:
0012234
Arg of perigee: 347
6775 deg
Mean anomaly: 12
4076 deg
Mean motion: 15
52626802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 316
Coasting Arc #5 (Orbit 1907)
---------------------------------------
Vector Time (GMT): 2013/067/12:20:01
915
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -557859
29 A = 6791319
95 meter
Y = -6317436
55 meter E =
0019378
Z = 2392591
62 I = 51
32648
XDOT = 5284
138616 Wp = 36
02359
YDOT = 1559
972395 meter/sec RA = 247
37846 deg
ZDOT = 5344
347356 TA = 350
85602
MA = 350
89126
Ha = 225
986 n
mi
Hp = 216
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1830247
02 X = -498797
23
Y = -20726497
85 feet Y = -6323344
41 meter
Z = 7849710
04 Z = 2390025
72
XDOT = 17336
412783 XDOT = 5240
341083
YDOT = 5118
019669 feet/sec YDOT = 1618
818598 meter/sec
ZDOT = 17533
948017 ZDOT = 5369
910160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1544460
88 X = 470751
68
Y = -20753525
27 feet Y = -6325674
50 meter
Z = 7839725
40 Z = 2389548
30
XDOT = 14642
323046 XDOT = 4462
980064
YDOT = 7761
599264 feet/sec YDOT = 2365
735456 meter/sec
ZDOT = 17640
148182 ZDOT = 5376
717166
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13067
57351396
00016717 00000-0 10270-3 0 9047
2 25544 51
6423 247
9758 0012003 351
2734 8
8208 15
52613882 19081
Satellite: ISS
Catalog Number: 25544
Epoch time: 13067
57351396 = yrday
fracday
Element set: 904
Inclination: 51
6423 deg
RA of node: 247
9758 deg
Eccentricity:
0012003
Arg of perigee: 351
2734 deg
Mean anomaly: 8
8208 deg
Mean motion: 15
52613882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1908
Checksum: 312
Coasting Arc #6 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2013/068/12:20:01
915
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -9799
87 A = 6788703
47 meter
Y = 5876705
57 meter E =
0012685
Z = -3414559
12 I = 51
33125
XDOT = -5526
257822 Wp = 18
09623
YDOT = -2670
196266 meter/sec RA = 242
38698 deg
ZDOT = -4572
509312 TA = 201
95318
MA = 202
00757
Ha = 226
168 n
mi
Hp = 215
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -32151
81 X = -58927
04
Y = 19280530
08 feet Y = 5876320
89 meter
Z = -11202621
80 Z = -3414726
75
XDOT = -18130
767131 XDOT = -5473
776815
YDOT = -8760
486437 feet/sec YDOT = -2731
701465 meter/sec
ZDOT = -15001
670972 ZDOT = -4599
227055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2796437
52 X = -852354
16
Y = 19075901
38 feet Y = 5814334
74 meter
Z = -11203951
67 Z = -3414964
47
XDOT = -15163
675970 XDOT = -4621
888436
YDOT = -11113
004791 feet/sec YDOT = -3387
243860 meter/sec
ZDOT = -15112
567147 ZDOT = -4606
310467
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13068
53898174
00016717 00000-0 10270-3 0 9055
2 25544 51
6427 243
1737 0012120 355
5415 4
5627 15
52651332 19230
Satellite: ISS
Catalog Number: 25544
Epoch time: 13068
53898174 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 243
1737 deg
Eccentricity:
0012120
Arg of perigee: 355
5415 deg
Mean anomaly: 4
5627 deg
Mean motion: 15
52651332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 299
Coasting Arc #7 (Orbit 1938)
---------------------------------------
Vector Time (GMT): 2013/069/12:20:01
915
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 683366
59 A = 6785899
86 meter
Y = -5237014
36 meter E =
0012995
Z = 4246957
88 I = 51
33676
XDOT = 5728
564546 Wp = 45
49707
YDOT = 3645
426904 meter/sec RA = 237
38966 deg
ZDOT = 3575
663939 TA = 7
87734
MA = 7
85695
Ha = 226
135 n
mi
Hp = 215
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2242016
37 X = 721246
98
Y = -17181805
65 feet Y = -5229160
15 meter
Z = 13933588
84 Z = 4250370
27
XDOT = 18794
503105 XDOT = 5670
005527
YDOT = 11960
062021 feet/sec YDOT = 3709
160382 meter/sec
ZDOT = 11731
180903 ZDOT = 3603
349590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4369637
66 X = 1331865
56
Y = -16755176
94 feet Y = -5106977
93 meter
Z = 13948343
74 Z = 4251455
17
XDOT = 15787
610072 XDOT = 4812
063550
YDOT = 13972
923856 feet/sec YDOT = 4258
947191 meter/sec
ZDOT = 11846
012181 ZDOT = 3610
664513
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13069
56880113
00016717 00000-0 10270-3 0 9064
2 25544 51
6423 238
0500 0011976 358
5649 1
5467 15
52669604 19394
Satellite: ISS
Catalog Number: 25544
Epoch time: 13069
56880113 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 238
0500 deg
Eccentricity:
0011976
Arg of perigee: 358
5649 deg
Mean anomaly: 1
5467 deg
Mean motion: 15
52669604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1939
Checksum: 322
Coasting Arc #8 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2013/070/12:20:01
915
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1434884
75 A = 6783501
18 meter
Y = 4517935
70 meter E =
0019634
Z = -4868636
01 I = 51
34745
XDOT = -5789
407208 Wp = 37
73379
YDOT = -4406
075556 meter/sec RA = 232
39034 deg
ZDOT = -2372
312777 TA = 208
82317
MA = 208
93178
Ha = 226
350 n
mi
Hp = 215
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4707627
15 X = -1461648
41
Y = 14822623
70 feet Y = 4501739
56 meter
Z = -15973215
26 Z = -4875672
13
XDOT = -18994
118138 XDOT = -5728
183340
YDOT = -14455
628463 feet/sec YDOT = -4470
474378 meter/sec
ZDOT = -7783
178401 ZDOT = -2400
287481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6251904
41 X = -1905580
47
Y = 14206836
63 feet Y = 4330243
80 meter
Z = -16002968
99 Z = -4877704
95
XDOT = -16157
739578 XDOT = -4924
879024
YDOT = -16045
593517 feet/sec YDOT = -4890
696904 meter/sec
ZDOT = -7899
143685 ZDOT = -2407
658995
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13070
53424664
00016717 00000-0 10270-3 0 9079
2 25544 51
6436 233
2485 0012073 3
1543 356
9683 15
52683943 19548
Satellite: ISS
Catalog Number: 25544
Epoch time: 13070
53424664 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 233
2485 deg
Eccentricity:
0012073
Arg of perigee: 3
1543 deg
Mean anomaly: 356
9683 deg
Mean motion: 15
52683943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 311
Coasting Arc #9 (Orbit 1969)
---------------------------------------
Vector Time (GMT): 2013/071/12:20:01
915
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2282983
10 A = 6781923
12 meter
Y = -3676883
56 meter E =
0010962
Z = 5215977
03 I = 51
36163
XDOT = 5722
908891 Wp = 24
23725
YDOT = 5003
160396 meter/sec RA = 227
38563 deg
ZDOT = 1031
043955 TA = 55
90644
MA = 55
80247
Ha = 226
381 n
mi
Hp = 215
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7490102
02 X = 2298591
51
Y = -12063266
26 feet Y = -3651265
74 meter
Z = 17112785
53 Z = 5227105
93
XDOT = 18775
947805 XDOT = 5661
528652
YDOT = 16414
568229 feet/sec YDOT = 5066
814526 meter/sec
ZDOT = 3382
690142 ZDOT = 1058
695255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8505120
13 X = 2592360
61
Y = -11299846
82 feet Y = -3444193
31 meter
Z = 17159482
60 Z = 5230210
30
XDOT = 16273
387712 XDOT = 4960
128575
YDOT = 17514
444737 feet/sec YDOT = 5338
402756 meter/sec
ZDOT = 3497
257762 ZDOT = 1065
964166
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13071
56404189
00016717 00000-0 10270-3 0 9084
2 25544 51
6434 228
1243 0012117 6
4146 353
7158 15
52683511 19706
Satellite: ISS
Catalog Number: 25544
Epoch time: 13071
56404189 = yrday
fracday
Element set: 908
Inclination: 51
6434 deg
RA of node: 228
1243 deg
Eccentricity:
0012117
Arg of perigee: 6
4146 deg
Mean anomaly: 353
7158 deg
Mean motion: 15
52683511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1970
Checksum: 294
Coasting Arc #10 (Orbit 1984)
---------------------------------------
Vector Time (GMT): 2013/072/12:20:01
915
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3145205
45 A = 6781482
86 meter
Y = 2859194
13 meter E =
0020384
Z = -5298287
79 I = 51
38331
XDOT = -5452
126043 Wp = 56
81829
YDOT = -5360
361943 meter/sec RA = 222
38379 deg
ZDOT = 355
759304 TA = 216
52245
MA = 216
66164
Ha = 226
491 n
mi
Hp = 214
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10318915
50 X = -3151206
26
Y = 9380558
17 feet Y = 2823988
13 meter
Z = -17382833
97 Z = -5313581
85
XDOT = -17887
552635 XDOT = -5393
508293
YDOT = -17586
489314 feet/sec YDOT = -5421
003246 meter/sec
ZDOT = 1167
189317 ZDOT = 329
416651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10917021
88 X = -3327508
27
Y = 8547877
40 feet Y = 2605393
03 meter
Z = -17446782
81 Z = -5317779
40
XDOT = -15833
742699 XDOT = -4826
124775
YDOT = -18142
158939 feet/sec YDOT = -5529
730045 meter/sec
ZDOT = 1058
095647 ZDOT = 322
507553
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13072
52946257
00016717 00000-0 10270-3 0 9099
2 25544 51
6447 223
3235 0012092 10
5139 349
6263 15
52723934 19859
Satellite: ISS
Catalog Number: 25544
Epoch time: 13072
52946257 = yrday
fracday
Element set: 909
Inclination: 51
6447 deg
RA of node: 223
3235 deg
Eccentricity:
0012092
Arg of perigee: 10
5139 deg
Mean anomaly: 349
6263 deg
Mean motion: 15
52723934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1985
Checksum: 312
Coasting Arc #11 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2013/073/12:20:01
915
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4044154
52 A = 6782534
39 meter
Y = -1995398
24 meter E =
0016482
Z = 5063659
96 I = 51
41000
XDOT = 4971
627433 Wp = 26
69392
YDOT = 5566
395427 meter/sec RA = 217
38068 deg
ZDOT = -1760
457356 TA = 80
47993
MA = 80
29370
Ha = 226
601 n
mi
Hp = 214
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13268223
50 X = 4041569
06
Y = -6546582
16 feet Y = -1950187
73 meter
Z = 16613057
60 Z = 5083300
06
XDOT = 16311
113626 XDOT = 4917
565125
YDOT = 18262
452188 feet/sec YDOT = 5621
688775 meter/sec
ZDOT = -5775
778726 ZDOT = -1736
437745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13542720
29 X = 4127821
14
Y = -5724378
71 feet Y = -1744790
63 meter
Z = 16695010
97 Z = 5088639
34
XDOT = 14776
393851 XDOT = 4503
844846
YDOT = 18244
085679 feet/sec YDOT = 5560
797315 meter/sec
ZDOT = -5676
366476 ZDOT = -1730
156502
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13073
55923326
00016717 00000-0 10270-3 0 9107
2 25544 51
6448 218
1995 0012147 14
4296 345
7200 15
52692119 20011
Satellite: ISS
Catalog Number: 25544
Epoch time: 13073
55923326 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 218
1995 deg
Eccentricity:
0012147
Arg of perigee: 14
4296 deg
Mean anomaly: 345
7200 deg
Mean motion: 15
52692119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 292
Coasting Arc #12 (Orbit 2015)
---------------------------------------
Vector Time (GMT): 2013/074/12:20:01
915
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4856887
02 A = 6784378
71 meter
Y = 1241270
50 meter E =
0015486
Z = -4578745
14 I = 51
44248
XDOT = -4276
457663 Wp = 58
60985
YDOT = -5580
707570 meter/sec RA = 212
38533 deg
ZDOT = 3038
851431 TA = 241
79997
MA = 241
95645
Ha = 226
637 n
mi
Hp = 214
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15934668
71 X = -4848163
89
Y = 4072409
77 feet Y = 1187005
95 meter
Z = -15022129
74 Z = -4602318
43
XDOT = -14030
372909 XDOT = -4228
497087
YDOT = -18309
408039 feet/sec YDOT = -5628
261084 meter/sec
ZDOT = 9969
985011 ZDOT = 3018
193948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16006363
71 X = -4878739
66
Y = 3366430
85 feet Y = 1026088
12 meter
Z = -15120384
72 Z = -4608693
26
XDOT = -13022
209046 XDOT = -3969
169317
YDOT = -17747
082117 feet/sec YDOT = -5409
310629 meter/sec
ZDOT = 9884
561049 ZDOT = 3012
814208
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13074
52462847
00016717 00000-0 10270-3 0 9112
2 25544 51
6457 213
3984 0012180 17
1840 342
9722 15
52742061 20164
Satellite: ISS
Catalog Number: 25544
Epoch time: 13074
52462847 = yrday
fracday
Element set: 911
Inclination: 51
6457 deg
RA of node: 213
3984 deg
Eccentricity:
0012180
Arg of perigee: 17
1840 deg
Mean anomaly: 342
9722 deg
Mean motion: 15
52742061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2016
Checksum: 290
Coasting Arc #13 (Orbit 2031)
---------------------------------------
Vector Time (GMT): 2013/075/12:20:01
915
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5607009
84 A = 6787161
98 meter
Y = -492247
73 meter E =
0020310
Z = 3789815
22 I = 51
47828
XDOT = 3332
952385 Wp = 51
08695
YDOT = 5484
860622 meter/sec RA = 207
39435 deg
ZDOT = -4190
991411 TA = 83
36224
MA = 83
13111
Ha = 226
745 n
mi
Hp = 214
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18395701
57 X = 5593687
63
Y = -1614985
99 feet Y = -429620
71 meter
Z = 12433776
98 Z = 3817021
27
XDOT = 10934
883154 XDOT = 3291
730501
YDOT = 17994
949547 feet/sec YDOT = 5521
900875 meter/sec
ZDOT = -13749
971822 ZDOT = -4174
900920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18355645
00 X = 5594800
60
Y = -1117903
05 feet Y = -340736
85 meter
Z = 12547087
92 Z = 3824352
40
XDOT = 10447
081082 XDOT = 3184
270314
YDOT = 16947
021917 feet/sec YDOT = 5165
452280 meter/sec
ZDOT = -13683
542559 ZDOT = -4170
743772
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13075
55437229
00016717 00000-0 10270-3 0 9123
2 25544 51
6457 208
2751 0012187 21
3351 338
8309 15
52747464 20325
Satellite: ISS
Catalog Number: 25544
Epoch time: 13075
55437229 = yrday
fracday
Element set: 912
Inclination: 51
6457 deg
RA of node: 208
2751 deg
Eccentricity:
0012187
Arg of perigee: 21
3351 deg
Mean anomaly: 338
8309 deg
Mean motion: 15
52747464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2032
Checksum: 302
Coasting Arc #14 (Orbit 2046)
---------------------------------------
Vector Time (GMT): 2013/076/12:20:01
915
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6165064
54 A = 6789791
77 meter
Y = -106742
01 meter E =
0016237
Z = -2832553
70 I = 51
51552
XDOT = -2230
551527 Wp = 34
84970
YDOT = -5289
844715 meter/sec RA = 202
41224 deg
ZDOT = 5081
595788 TA = 292
92261
MA = 293
09390
Ha = 226
821 n
mi
Hp = 213
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20226589
70 X = -6149652
96
Y = -350203
46 feet Y = -175597
73 meter
Z = -9293155
17 Z = -2862465
55
XDOT = -7318
082438 XDOT = -2195
918575
YDOT = -17355
133580 feet/sec YDOT = -5314
594042 meter/sec
ZDOT = 16671
902193 ZDOT = 5070
844581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20164460
53 X = -6146127
57
Y = -549632
80 feet Y = -167528
08 meter
Z = -9417682
39 Z = -2870509
59
XDOT = -7289
429727 XDOT = -2221
818181
YDOT = -15955
847139 feet/sec YDOT = -4863
342208 meter/sec
ZDOT = 16627
675889 ZDOT = 5068
115611
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13076
51974331
00016717 00000-0 10270-3 0 9131
2 25544 51
6463 203
4733 0012381 24
0620 336
1108 15
52767635 20470
Satellite: ISS
Catalog Number: 25544
Epoch time: 13076
51974331 = yrday
fracday
Element set: 913
Inclination: 51
6463 deg
RA of node: 203
4733 deg
Eccentricity:
0012381
Arg of perigee: 24
0620 deg
Mean anomaly: 336
1108 deg
Mean motion: 15
52767635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2047
Checksum: 285
Coasting Arc #15 (Orbit 2062)
---------------------------------------
Vector Time (GMT): 2013/077/12:20:01
915
Vector Time (MET): N/A
Weight (LBS) : 923412
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6552390
04 A = 6791987
72 meter
Y = 687273
08 meter E =
0018960
Z = 1647093
75 I = 51
55164
XDOT = 920
294398 Wp = 75
79157
YDOT = 5034
220499 meter/sec RA = 197
43662 deg
ZDOT = -5701
917847 TA = 86
16808
MA = 85
95132
Ha = 226
919 n
mi
Hp = 213
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21497342
64 X = 6536216
70
Y = 2254832
93 feet Y = 760455
73 meter
Z = 5403850
88 Z = 1678885
24
XDOT = 3019
338577 XDOT = 891
630578
YDOT = 16516
471455 feet/sec YDOT = 5044
351064 meter/sec
ZDOT = -18707
079552 ZDOT = -5697
517197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21479596
86 X = 6546981
12
Y = 2097491
29 feet Y = 639315
35 meter
Z = 5536159
81 Z = 1687421
51
XDOT = 3408
830222 XDOT = 1039
011452
YDOT = 14925
368429 feet/sec YDOT = 4549
252297 meter/sec
ZDOT = -18689
265036 ZDOT = -5696
487983
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13077
54946014
00016717 00000-0 10270-3 0 9143
2 25544 51
6461 198
3503 0012316 28
2625 331
9193 15
52800852 20638
Satellite: ISS
Catalog Number: 25544
Epoch time: 13077
54946014 = yrday
fracday
Element set: 914
Inclination: 51
6461 deg
RA of node: 198
3503 deg
Eccentricity:
0012316
Arg of perigee: 28
2625 deg
Mean anomaly: 331
9193 deg
Mean motion: 15
52800852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2063
Checksum: 295
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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